View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 56337U 26145.59095736 +.00000000 +00000-0 -10524-2 0 00004
2 56337 97.4447 145.5034 0001813 116.6756 243.4657 15.05552963 00
| Epoch (UTC): | 25 May 2026 14:10:58 |
| Eccentricity: | 0.0001813 |
| inclination: | 97.4447° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.5034° |
| argument of perigee: | 116.6756° |
| revolutions per day: | 15.05552963 |
| mean anomaly at epoch: | 243.4657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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